Mechanical behaviour of bimodulus laminated plates

Papazoglou, VJ; Tsouvalis, NG

dc.contributor.author	Papazoglou, VJ	en
dc.contributor.author	Tsouvalis, NG	en
dc.date.accessioned	2014-03-01T01:08:25Z
dc.date.available	2014-03-01T01:08:25Z
dc.date.issued	1991	en
dc.identifier.issn	0263-8223	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/10482
dc.subject.classification	Materials Science, Composites	en
dc.subject.other	Composite Materials--Stresses	en
dc.subject.other	Laminated Products--Composites	en
dc.subject.other	Bimodulus Laminated Plates	en
dc.subject.other	Higher Order Shear Deformation Theory	en
dc.subject.other	Plates	en
dc.title	Mechanical behaviour of bimodulus laminated plates	en
heal.type	journalArticle	en
heal.identifier.primary	10.1016/0263-8223(91)90057-6	en
heal.identifier.secondary	http://dx.doi.org/10.1016/0263-8223(91)90057-6	en
heal.language	English	en
heal.publicationDate	1991	en
heal.abstract	A new analytical method for the prediction of the mechanical behaviour of laminates consisting of layers having different properties in tension and compression is proposed in this paper. As a case study, bending of simply supported, multilayered, unsymmetric, specially orthotropic laminates under various types of lateral loads is considered. The underlying bending theory used is a higher-order shear deformation theory. With the proposed method, laminates having more than two layers, not necessarily in an antisymmetric stacking sequence, can be analyzed. The validity of the new method is confirmed by comparing its results with the ones of other simpler theories. Finally, as an example, deflections, strains and stresses are calculated for a five-layer, unsymmetric, specially-orthotropic laminate. © 1990.	en
heal.publisher	ELSEVIER SCI LTD	en
heal.journalName	Composite Structures	en
dc.identifier.doi	10.1016/0263-8223(91)90057-6	en
dc.identifier.isi	ISI:A1991EH28700001	en
dc.identifier.volume	17	en
dc.identifier.issue	1	en
dc.identifier.spage	1	en
dc.identifier.epage	22	en